DEVICE FOR AIDING THE PILOTING OF AN AIRCRAFT DURING AN APPROACH PHASE FOR THE PURPOSE OF LANDING

The device has a control system (10) e.g. flight control unit, including control units (11A-11n) for controlling a pilot of an aircraft in two guiding modes. A calculation system (7) determines vertical and lateral deviations related to the guiding modes. A guidance system (8) automatically carries...

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Bibliographic Details
Main Authors HUYNH, JEAN-PHILIPPE, ROUQUETTE, PATRICE
Format Patent
LanguageEnglish
French
German
Published 05.11.2008
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
CONTROLLING
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
PHYSICS
REGULATING
SIGNALLING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TRAFFIC CONTROL SYSTEMS
TRANSPORTING
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Summary:The device has a control system (10) e.g. flight control unit, including control units (11A-11n) for controlling a pilot of an aircraft in two guiding modes. A calculation system (7) determines vertical and lateral deviations related to the guiding modes. A guidance system (8) automatically carries out transition between the two guiding modes corresponding to initial and terminal phases, respectively. A display system (9) displays activation of the control system on navigation and primary flight displays (12, 13).
Bibliography:Application Number: EP20070730970